Consider the following free-body digram of a beam.10 N-mA•B5m5mWhat is Cy?а. ОO b. None of the aboveOC. 1 N.mO d. 10 N.m

Consider the free-body diagram of the beam.Write the equilibrium equation for the sum of vertical forces. ∑Fy=0Cy=0 Therefore, option (a) is correct.

Answered: Consider the following free-body digram…

Engineering

Civil Engineering

Consider the following free-body digram of a beam. 10 N-m C. M Sm Sm What is Cy?

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Related questions

Q: The beam cross section shown below has been proposed for a short pedestrian bridge. The cross…

Q: The bear cross section shown below has been proposed for a short pedestrian bridge. The cross…

A: Determonation of shear stress at H

Q: A ruler is clamped clamped at weight 0-36 ку weight is at = deflection at deflection at It is x=17cm…

A: A ruler is clamped at x=3 cm and x=30 cm,Weight of 0.36 kg is concentrated at x=17 cmDeflection at…

Q: a) Determine thę centroid location (measured upward from the bottom), in mm rounded to the nearest…

Q: The piece of plastic is originally rectangular. Calculate the shear strain Yxy at corners A and B if…

A: For small angles.

Q: The piece of rubber is originally rectangular. Calculate the average shear strain Yxy at A if the…

Q: A circular steel rod AB of diameter d1,length L and modulus of rigidity G is loaded as shown is…

Q: Please calculate the deflection-y at point 5, and the deflection-x at point 2 based on the following…

A: ####Calculation of deflection Y at 5 and Deflection X at 2 Using Unit load Method of Analysis ####

Q: ows an elastic be igidity EI and deflection v(x) d by an equation

Q: The figure shows a cutaway view of an assembly in which a solid bronze [G= 6,500 ksi] rod (1) is…

Q: Three steel rods, each having a cross-sectional area of 500 mm2, are assembled in a symmetrical…

Q: 5.15 A beam in bending has the cross section of an L3 × 2 × 0.25 in unequal leg steel angle. A…

Q: Three round bars welded together axially loaded as shown. Find the normal are stress in each bar if…

A: Stress is defined as the force acting per unit area of a bar. The stress in a bar is directly…

Q: Determine the structure stiffness matrix S for the beam shown.

Question

Consider the following free-body digram of a beam.
10 N-m
A
•B
5m
5m
What is Cy?
а. О
O b. None of the above
OC. 1 N.m
O d. 10 N.m

Expert Solution

This question has been solved!

Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.

This is a popular solution!

SEE SOLUTION Check out a sample Q&A here

Step 1

VIEW

Step 2

VIEW

Trending now

This is a popular solution!

Step by step

Solved in 2 steps with 1 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, civil-engineering and related others by exploring similar questions and additional content below.

Similar questions

A cantilever beam is subjected to a uniformly-distributed load with an intensity of w. The beam has a Young's modulus of Eo, a length of 1 and 2nd moment of area of Iz. A W |↓↓↓↓↓↓↓↓↓↓↓↓↓↓ +x- B R
A beam has a cross section show below. If the stress at point P is 30Kpa , calculate the value for the shear force V. can you please show details? especially how to calculate the moment of inertia. I got a first response but I got confuse how the person use the parameters to calculate INERTIA
The 16 x 22 x 25-mm rubber blocks shown are used in a double U shear mount to isolate the vibration of a machine from its supports. An applied load of P = 238 N causes the upper frame to be deflected downward by 4 mm. Determine the shear modulus G of the rubber blocks. Double U anti-vibration shear mount 25 Rubber block dimensions Shear deformation of blocks O 0.745 MPa O 0.883 MPa O 1.140 MPa
= 29,000 For the structure and loading shown below, find the lateral deflection at the top. Use E ksi and I = 250 in4 for all members. Note that in frames, we neglect axial deformation, so you can calculate the deflection at either of the upper corners; the answer will be the same. t. 201 8K 10! 1. What is the deflection at the top in inches (two decimal places) ot
The rigid bar AOB is pinned at O and connected to aluminum and steel rods. If the bar is horizontal at a given temperature, determine the ratio of the areas of the two rods so that the bar will be horizontal at any temperature. Neglect the mass of the bar. 2m 6m A Steel E = 200 GPa a = 11.7 x 10-6/°C L=8 m Aluminum E = 70 GPa a = 23.0 × 10-6/°C L = 8 m
Non uniform beam Flexural Rigidity that is _y(x) = fixed support on left Simple support 07 right P 2.26 meters long 141702000 6441 + 100x Find the deflection of the bean if it is uniform distributed load of under a 92 N/m TPE Nm²
determine the maximum displacement of the beam in the figure shown .
А L B 425 mm C 1,000 mm V P A steel bar (1) and an Aluminum bar (2) are connected to a rigid angle ACD. Assuming: • Steel [E = 200 GPa] bar (1) is 6mm x 40mm x 600mm long. • Aluminum [E = 70 GPa] bar (2) is 10mm x 40mm x 600mm long. Poisson's ratio, v = 0.35 • A distance L of 500mm. a)Determine the force P (in kN) required to stretch the Aluminum bar by 1mm. Enter the force, P, into the d21 answer box (in kN, 3 sig digs). b) Determine the final width and thickness of the Aluminum bar. (1) Your Answer:
Two torque as shown are applied on a compound shaft of aluminum segment and a steel. Determine the maximum permissible value of T subjected to the following conditions: T, s 90MPA, T. S 65MPA and the angle of rotation of the free end limited to 11°. Use GS 84 GPa and Ga = 27 GPa. %3D %3D 75 mm Aluminum Steel 50 mm 2 m 1.5 m
the last digit of i.d number is 916 method of members/fram
Elementary beam theory predicts that the axial bending stress ox in a prismatic beam is given by: ox = (M.I,M,L)y+(M,I.-M.I.) (1,1₂-13/2) where My and M₂ are bending moments applied to a cross-section, and where ly, lz and lyz are second moments of area in the usual notation (Oxyz is a Cartesian coordinate system in which the x axis corresponds to the centroidal axis of the beam). (iii) A Z--section beam has the cross-section shown overleaf (see Figure QB2). The second moments of area of the section about the y and z axes are given as;; ly = 1.12x106mm² and I₂ = 2.87x106 mm4. Show that lyz = 1.35x106 mm² (use the parallel axis theorem). 100 60 10 y -10 10 60 Figure QB2 N (iv) Bending moments Mz = 2.0 kNm and My = 0 kNm act on a cross- -section of the beam of part (iii). Obtain an expression for the bending stress and sketch the orientation of the neutral axis with reference to the y and z axes. What is the maximum tensile value of the axial bending stress and where does it occur?
I WOULD LIKE TO KNOW HOW TO SOLVE THE TWO PROBLEMS STEP BY STEP IN THE IMAGE ATTACHED